| 液氧/煤油发动机试验系统 |
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| 引用本文： | 李伟民.液氧/煤油发动机试验系统[J].火箭推进,2005,31(6):50-56. |
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| 作者姓名： | 李伟民 |
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| 作者单位： | 西安航天动力试验技术研究所,陕西,西安,710100 |
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| 摘 要： | 设计并建立了液氧／煤油发动机发生器-涡轮泵联动装置和整机试验系统。详细介绍了推进剂供应系统、煤油回流系统、试验工艺辅助系统、控制系统的组成及试验能力，重点论述了关键试验工艺技术，主要包括启动技术、增压技术、试车工艺、安全措施。
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| 关 键 词： | 液氧/煤油发动机 系统组成 试验能力 工艺 |
| 文章编号： | (2005)06-0050-07 |
| 收稿时间： | 2005-03-07 |
| 修稿时间： | 2005-03-15 |
LOX/kerosene rocket engine test system |
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| Li Weimin.LOX/kerosene rocket engine test system[J].Journal of Rocket Propulsion,2005,31(6):50-56. |
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| Authors: | Li Weimin |
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| Abstract: | A gas generator-turbopump test device and an overall engine test system for LOX/kerosene rocket engine were developed. System composition and test ability of propellant feed system, kerosene return system, control system and auxiliary system for technique test were described in detail. Key test techniques such as start technology, pressurization technology, test technique and safety measures were primarily introduced. |
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| Keywords: | LOX/kerosene engine system composition test ability technique |
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